Application of Metallic Materials for Aircraft Structures in the Temperature Range 600 to 1100 F North American Aviation, Incorporated

Format:

Conference/Event

Author/Creator:

Huffman, James W., author.

Conference Name:

This paper was presented at the Aircraft Research Seminar held by the SAE Southern California Section at the University of California

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1956

Summary:

A BRIEF review is presented of a portion of the available strength property data for a few representative alloys which find use in airframe structural components in the range from 600 to 1100 F. Several modes of behavior are illustrated, and some general principles regarding the interpretation and use of said data for design purposes are discussed

Notes:

Vendor supplied data

Publisher Number:

560002

Access Restriction:

Restricted for use by site license